Automatic approach procedure of a flying vehicle on a mobile platform using backstepping controller

Q2 Engineering INCAS Bulletin Pub Date : 2022-12-02 DOI:10.13111/2066-8201.2022.14.4.5
Florin Costache, S. Nichifor, M. Costea, A. Ionita
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Abstract

This paper presents the automatic approach procedure of a flying vehicle, attached to an ABB 7600 robot, and a mobile platform, attached to a Stewart platform. Due to a nonlinear dynamic behavior, it is necessary to implement complex control, stabilization and guidance schemes. The proposed solution for this system includes the development of an algorithm based on a backstepping control method, the controller design methodology being based on Lyapunov's stability theory. The proposed command law requires that the states are known, but it is also necessary to introduce a series of state estimators. Tracking a mobile platform is critical in surveillance, reconnaissance and tracking missions, with the control methodology defining a clear distinction between translational and rotational dynamics. The proposed algorithm is developed by separating two types of states involving an inverse kinematics, known as algebraic kinematics, in which the dynamic movements of the two pieces of equipment are used. The dynamics of the ABB 7600 robot involves a movement with seven degrees of freedom, while the Stewart platform can be used with a movement of six degrees of freedom. The proposed algorithm is implemented in both Matlab software and experimental testing. This paper provides results in terms of generating dynamics for both devices that can be used for simulating different scenarios of aerospace missions.
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基于backstepping控制器的飞行器在移动平台上的自动进近过程
本文介绍了附着在ABB 7600机器人上的飞行器和附着在Stewart平台上的移动平台的自动接近过程。由于其非线性动态特性,需要实现复杂的控制、稳定和制导方案。该系统的拟议解决方案包括开发一种基于反推控制方法的算法,控制器设计方法基于李雅普诺夫稳定性理论。所提出的命令定律要求状态是已知的,但也有必要引入一系列状态估计器。跟踪移动平台在监视、侦察和跟踪任务中至关重要,控制方法明确区分了平移和旋转动力学。所提出的算法是通过分离两种类型的状态来开发的,这两种状态涉及反向运动学,称为代数运动学,其中使用两件设备的动态运动。ABB 7600机器人的动力学涉及七个自由度的运动,而Stewart平台可以使用六个自由度。该算法已在Matlab软件和实验测试中实现。本文提供了两种设备的动力学生成结果,可用于模拟航空航天任务的不同场景。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
INCAS Bulletin
INCAS Bulletin Engineering-Aerospace Engineering
自引率
0.00%
发文量
50
审稿时长
8 weeks
期刊介绍: INCAS BULLETIN is a scientific quartely journal published by INCAS – National Institute for Aerospace Research “Elie Carafoli” (under the aegis of The Romanian Academy) Its current focus is the aerospace field, covering fluid mechanics, aerodynamics, flight theory, aeroelasticity, structures, applied control, mechatronics, experimental aerodynamics, computational methods. All submitted papers are peer-reviewed. The journal will publish reports and short research original papers of substance. Unique features distinguishing this journal: R & D reports in aerospace sciences in Romania The INCAS BULLETIN of the National Institute for Aerospace Research "Elie Carafoli" includes the following sections: 1) FULL PAPERS. -Strength of materials, elasticity, plasticity, aeroelasticity, static and dynamic analysis of structures, vibrations and impact. -Systems, mechatronics and control in aerospace. -Materials and tribology. -Kinematics and dynamics of mechanisms, friction, lubrication. -Measurement technique. -Aeroacoustics, ventilation, wind motors. -Management in Aerospace Activities. 2) TECHNICAL-SCIENTIFIC NOTES and REPORTS. Includes: case studies, technical-scientific notes and reports on published areas. 3) INCAS NEWS. Promote and emphasise INCAS technical base and achievements. 4) BOOK REVIEWS.
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